Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits
The problem of relative motion control for spacecraft formation flying in eccentric orbits is considered in this paper. Due to the presence of nonlinear dynamics and external disturbances, a robust fuzzy sliding mode controller is developed. The slopes of sliding surfaces of the conventional sliding...
Kaydedildi:
| Asıl Yazarlar: | , |
|---|---|
| Materyal Türü: | Artigo |
| Dil: | Persa |
| Baskı/Yayın Bilgisi: |
Aerospace Research Institute
2014-04-01
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| Seri Bilgileri: | فصلنامه علوم و فناوری فضایی |
| Konular: | |
| Online Erişim: | https://jsst.ias.ir/article_14497_6b16ff082a514d99af2efbb9900787f1.pdf |
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